Experimental deformation of hornblende and amphibolite

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086 0 ‡aD 301.45/39:299
088 ‡aAD 0690511
088 ‡aAFCRL 69-68
100 1 ‡aRooney, Thomas Peter, ‡d1932-
245 1 0 ‡aExperimental deformation of hornblende and amphibolite / ‡cThomas P. Rooney, Robert E. Riecker.
264 1 ‡aL.G. Hanscom Field, Bedford, Massachusetts : ‡bAir Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, ‡c1969.
300 ‡avi, 24 pages : ‡billustrations ; ‡c28 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
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490 0 ‡aAFCRL ; ‡v69-68
490 0 ‡aEnvironmental Research Papers ; ‡vNo. 299
500 ‡aAmphibolite and hornblende were deformed in shear type apparatus, with over 200 tests run at conditions to 80 kb and 900C. Intragranular deformation was observed as undulatory extinction, deformation twins and kink bands. Kink band geometry tentatively establishes the slip system as T = (100), t = c. Shear strength at low temperatures, high pressures, and fast strain rates (27C, 40-50 kb, 0.10/sec), ranges between 11.6 and 12.8 kb for both hornblende and amphibolite. At 900C, shear strength decreases to less than 5 kb. Only thermally activated weakening manifests in shear tests. (Author).
500 ‡aResearch supported by the Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, L.G. Hanscom Field, Bedford, Massachusetts.
500 ‡aTerrestrial Sciences Laboratory Project 8623.
500 ‡aAD0690511 (from http://www.dtic.mil).
500 ‡a"February 1969."
504 ‡aIncludes bibliographical references (pages 23-24).
538 ‡aMode of access: Internet.
650 7 ‡aRock deformation. ‡2fast ‡0(OCoLC)fst01099157
650 7 ‡aHornblende. ‡2fast ‡0(OCoLC)fst00960312
650 7 ‡aAmphibolite. ‡2fast ‡0(OCoLC)fst00807961
650 0 ‡aAmphibolite.
650 0 ‡aHornblende.
650 0 ‡aRock deformation.
700 1 ‡aRiecker, Robert E.
710 2 ‡aAir Force Cambridge Research Laboratories (U.S.)
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095132760
CID ‡a102198112
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